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T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

FRONT. REAR. T700 ENGINE(1546 SHP) – RIGHT HAND SIDE. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit. FRONT. REAR. T700 ENGINE(1546 SHP) – RIGHT HAND SIDE. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal

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T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

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  1. FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  2. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  3. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  4. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  5. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  6. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  7. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  8. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS PAS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  9. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS PAS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  10. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P2.5) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS PAS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  11. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS PAS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  12. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  13. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  14. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec Transient Np Overspeed Sensor – 106+/-1% T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  15. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec Transient Np Overspeed Sensor – 106+/-1% T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  16. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec Transient Np Overspeed Sensor – 106+/-1% Np Turbine Min 91% except idle/transient 95-101% Cont 101-105% Transient 105-107% 12 Sec Transient (avoid 20-40 and 60-90%) -2 STAGE -100% = 20900RPM -Uses 25% of combustion energy T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  17. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec Transient Np Overspeed Sensor – 106+/-1% Np Turbine Min 91% except idle/transient 95-101% Cont 101-105% Transient 105-107% 12 Sec Transient (avoid 20-40 and 60-90%) -2 STAGE -100% = 20900RPM -Uses 25% of combustion energy T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  18. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec TransientNp Overspeed Sensor – 106+/-1% Np Turbine Min 91% except idle/transient 95-101% Cont 101-105% Transient 105-107% 12 Sec Transient (avoid 20-40 and 60-90%) -2 STAGE -100% = 20900RPM -Uses 25% of combustion energy NG Turbine 0-99% Cont 99-102% 30 min 102-105% 10 sec -2 STAGE -29000 (idle 63%) –44700 RPM (100%) -Uses 75% of combustion energy T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  19. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec Transient Np Overspeed Sensor – 106+/-1% Np Turbine Min 91% except idle/transient 95-101% Cont 101-105% Transient 105-107% 12 Sec Transient (avoid 20-40 and 60-90%) -2 STAGE -100% = 20900RPM -Uses 25% of combustion energy NG Turbine 0-99% Cont 99-102% 30 min 102-105% 10 sec -2 STAGE -29000 (idle 63%) –44700 RPM (100%) -Uses 75% of combustion energy T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  20. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec TransientNp Overspeed Sensor – 106+/-1% Np Turbine Min 91% except idle/transient 95-101% Cont 101-105% Transient 105-107% 12 Sec Transient (avoid 20-40 and 60-90%) -2 STAGE -100% = 20900RPM -Uses 25% of combustion energy NG Turbine 0-99% Cont 99-102% 30 min 102-105% 10 sec -2 STAGE -29000 (idle 63%) –44700 RPM (100%) -Uses 75% of combustion energy • Axial Compressor • -5 STAGE • Comp Ratio of Axial Comp 7:1 • Comp ratio of both Axial and Centr 17:1 T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  21. TGT (T4.5) Thermocouples(7) 538-775 Deg C Normal 775-850 Deg 30 min Limit 850 deg – Start Abort 850 – 886 deg 12 Sec Limit • Centrifugal Compressor • Single Stage - 5th Stage Air(P3) • air for AISBV • air for Eng Inlet Anti Ice • Air for Pneumatic Manifold(X-bleed Start) • Air for purging • Air for Cockpit Heat and ERFS • Pneumatic Starter • for X-bleed start must have min 90%Ng, 100%Np and Eng Anti Ice Light Off. • At least 60 sec b/n each start cycle • 15 deg C and below • 2 consecutive start followed by 3 min rest then 2 addn starts followed by 30 mins • Above 15 deg C • -2 consecutive start cycles followed by 30 min rest • COMBUSTION LINER • 12 FUEL INJECTORS • 2 PRIMER NOZZLES • 2 IGNITORS PAS LDS FRONT REAR TQ Sensor 0 –100% Dual Cont 0 – 110% Single Cont 100-125% Dual 12 Sec Transient 110-135% Single 12 Sec Transient Np Overspeed Sensor – 106+/-1% Np Turbine Min 91% except idle/transient 95-101% Cont 101-105% Transient 105-107% 12 Sec Transient (avoid 20-40 and 60-90%) -2 STAGE -100% = 20900RPM -Uses 25% of combustion energy NG Turbine 0-99% Cont 99-102% 30 min 102-105% 12 sec -2 STAGE -29000 (idle 63%) –44700 RPM (100%) -Uses 75% of combustion energy • Axial Compressor • -5 STAGE • Comp Ratio of Axial Comp 7:1 • Comp ratio of both Axial and Centr 17:1 T700 ENGINE(1546 SHP) – RIGHT HAND SIDE

  22. T700 ENGINE – LEFT HAND SIDE FRONT REAR

  23. T700 ENGINE – LEFT HAND SIDE • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above FRONT REAR

  24. T700 ENGINE – LEFT HAND SIDE • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above FRONT REAR

  25. T700 ENGINE – LEFT HAND SIDE • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FRONT REAR

  26. T700 ENGINE – LEFT HAND SIDE • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FRONT REAR

  27. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FRONT REAR

  28. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FRONT REAR

  29. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) FRONT REAR

  30. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) FRONT REAR

  31. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) FRONT REAR

  32. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) FRONT REAR

  33. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR

  34. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR

  35. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Np SENSOR

  36. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Np SENSOR

  37. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Eng Inlet Anti Ice Port Np SENSOR

  38. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Eng Inlet Anti Ice Port Np SENSOR

  39. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Eng Inlet Anti Ice Port Eng Anti-Ice Np SENSOR

  40. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Eng Inlet Anti Ice Port Eng Anti-Ice Np SENSOR

  41. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Eng Inlet Anti Ice Port Eng Anti-Ice ECU (ECU Functions are….??) Np SENSOR

  42. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS FUEL INJECTORS(12) THERMO-COUPLE HARNESS (TGT) IGNITORS(2) FRONT REAR Eng Inlet Anti Ice Port Eng Anti-Ice • ECU: • Np Governing to maintain constant Power Turbine and Rotor RPM • Load Share Comparator(keeps tq within 5% by adjust low eng Np up to 3% • TGT Limit Amplifier(limits TGT to 837-849 deg), inop during Eng Start, Lockout, Compressor Stall and Alternator Failure • Tq Motor Amplifier – actuates Tq Motor in HMU to bias metering valve and also receives feedback signal from Linear Variable Differential Transducer in HMU • Np Overspeed Switch to actuate Overspeed Solenoid – backup power from AC Primary Bus • History Recorder – records TGT and Ng and is used to track life of GG and IPS (backup power from AC Primary Bus) • Conditioning and Transfer to cockpit of Tq and Np Signals. • Np Reference for Np Trim Switch 96-100% with Pilot Side having authority Np SENSOR

  43. T700 ENGINE – LEFT HAND SIDE ACTUATOR/CRANKSHAFT ASSEMBLY FOR VARIABLE GEOMETRY SYSTEM • AISBV • Actuates automatically to provide bleed functions at approx 88-92% Ng or 30% Tq • Will open below 88-92% Ng and close above IPS THERMO-COUPLE HARNESS (TGT) FUEL INJECTORS(12) IGNITORS(2) FRONT Eng Inlet Anti Ice Port Eng Anti-Ice • ECU: • Np Governing to maintain constant Power Turbine and Rotor RPM • Load Share Comparator(keeps tq within 5% by adjust low eng Np up to 3% • TGT Limit Amplifier(limits TGT to 837-849 deg), inop during Eng Start, Lockout, Compressor Stall and Alternator Failure • Tq Motor Amplifier – actuates Tq Motor in HMU to bias metering valve and also receives feedback signal from Linear Variable Differential Transducer in HMU • Np Overspeed Switch to actuate Overspeed Solenoid – backup power from AC Primary Bus • History Recorder – records TGT and Ng and is used to track life of GG and IPS (backup power from AC Primary Bus) • Conditioning and Transfer to cockpit of Tq and Np Signals. • Np Reference for Np Trim Switch 96-100% with Pilot Side having authority Np SENSOR

  44. T700 ENGINE – FRONT VIEW

  45. ALTERNATOR • -1 Winding for Ng Signal • 1 Winding for ECU Power • 1 Winding for Engine Ignition T700 ENGINE – FRONT VIEW

  46. ALTERNATOR • -1 Winding for Ng Signal • 1 Winding for ECU Power • 1 Winding for Engine Ignition T700 ENGINE – FRONT VIEW

  47. OIL TEMP/ PRESSURE SENSE (NOT VISIBLE) • Pressure Light on at 20 PSI • Temp Light on at 150 deg C • ALTERNATOR • -1 Winding for Ng Signal • 1 Winding for ECU Power • 1 Winding for Engine Ignition T700 ENGINE – FRONT VIEW

  48. OIL TEMP/ PRESSURE SENSE (NOT VISIBLE) • Pressure Light on at 20 PSI • Temp Light on at 150 deg C • ALTERNATOR • -1 Winding for Ng Signal • 1 Winding for ECU Power • 1 Winding for Engine Ignition T700 ENGINE – FRONT VIEW

  49. OIL PUMP • 6 Scavenge Elements • 1 Pressure Element • OIL TEMP/ PRESSURE SENSE (NOT VISIBLE) • Pressure Light on at 20 PSI • Temp Light on at 150 deg C • ALTERNATOR • -1 Winding for Ng Signal • 1 Winding for ECU Power • 1 Winding for Engine Ignition T700 ENGINE – FRONT VIEW

  50. OIL PUMP • 6 Scavenge Elements • 1 Pressure Element • OIL TEMP/ PRESSURE SENSE (NOT VISIBLE) • Pressure Light on at 20 PSI • Temp Light on at 150 deg C • ALTERNATOR • -1 Winding for Ng Signal • 1 Winding for ECU Power • 1 Winding for Engine Ignition T700 ENGINE – FRONT VIEW

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